ZHU Lin,YANG Xiu-bin,XU Chao,XU Ting-ting,JIANG Li.Analysis on the motion characteristics of dynamic aircraft by dual-line-array TDI CCD optical camera[J].Optoelectronics Letters,2020,16(1):1-6
Analysis on the motion characteristics of dynamic aircraft by dual-line-array TDI CCD optical camera
Author NameAffiliation
ZHU Lin Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033,
University of Chinese Academy of Sciences, Beijing 100049, China 
YANG Xiu-bin Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033,
National & Local United Engineering Research Center of Small Satellite Technology, Changchun 130033, China 
XU Chao Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033,
University of Chinese Academy of Sciences, Beijing 100049, China 
XU Ting-ting Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033,
University of Chinese Academy of Sciences, Beijing 100049, China 
JIANG Li Changchun University of Science and Technology, Changchun 130033, China 
Abstract:
      A time-differential imaging method using a dual-line-array time delayed and integration (TDI) CCD optical camera is proposed in this paper, precisely measuring the motion parameters of the dynamic aircraft. Firstly, based on the spatiotemporal information of the aircraft obtained by the optical satellites, the velocity on the image plane and the twice imaging time interval are calculated. The improved scale-invariant feature transform (SIFT) algorithm that integrates the aerodynamic configuration of the aircraft is proposed to extract the region of interest. After that, the geometric centers of the aircraft images are determined with the median method, and then the velocity vector of the aircraft can be obtained by synthesizing a variety of spatial parameters and mathematical techniques. Finally, using the snapshots of the dynamic aircraft in the area of Harbin captured by the commercial satellite JL-1, the calculated results are quite close to its actual motion characteristics, which verify our method. This paper plays a guiding role in the evaluation and surveillance of dynamic aircraft.
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